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PRELIMINARY DESIGN CONSIDERATIONS FOR ACCESS AND OPERATIONS IN EARTH-MOON L_1/L_2 ORBITS

机译:初步设计考虑到地球L_1 / L_2轨道中的访问和操作

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Within the context of manned spaceflight activities, Earth-Moon libration point orbits could support lunar surface operations and serve as staging areas for future missions to near-Earth asteroids and Mars. This investigation examines preliminary design considerations including Earth-Moon L_1/L_2 libration point orbit selection, transfers, and stationkeeping costs associated with maintaining a spacecraft in the vicinity of L_1 or L_2 for a specified duration. Existing tools for multi-body trajectory design, dynamical systems theory, and orbit maintenance are leveraged in this analysis to explore end-to-end concepts for manned missions to Earth-Moon libration points.
机译:在载人航天活动的背景下,地球 - 月亮的自由点轨道可以支持月球表面运营,并用作未来任务到近地球小行星和火星的暂存区域。该调查审查了与维护L_1或L_2附近的航天器相关联的初步设计考虑因素,包括与维护L_1或L_2附近的航天器相关的持续时间。在该分析中利用了多体轨迹设计,动态系统理论和轨道维护的现有工具,以探讨载人任务到地球加权点的端到端概念。

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